Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory期刊界 All Journals 搜尽天下杂志传播学术成果专业期刊搜索期刊信息化学术搜索

Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory

Authors:	A.?V.?Gorelov author-information" > author-information__contact u-icon-before" > mailto:a.gorelov-kai@yandex.ru" title=" a.gorelov-kai@yandex.ru" itemprop=" email" data-track=" click" data-track-action=" Email author" data-track-label=" " >Email author,E.?I.?Nikolaev,I.?N.?Sidorov

Affiliation:	1.Chistopol branch “Vostok”,Tupolev Kazan National Research Technical University,Tatarstan,Russia;2.PAO Kazan Helicopters,Tatarstan,Russia;3.Tupolev Kazan National Research Technical University,Tatarstan,Russia

Abstract:	Safety factors of the Ansat helicopter main rotor blade are determined in the root section at various flight modes with taking into account the possible damages.

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